A Note on the Use of Generalized Sundman Anomalies in the Numerical Integration of the Elliptical Orbital Motion

Table 2

Optimal for    in  Km and in .

0.00	1.539			0.50	1.671
0.05	1.561			0.55	1.681
0.10	1.578			0.60	1.692
0.15	1.593			0.65	1.704
0.20	1.606			0.70	1.718
0.25	1.618			0.75	1.735
0.30	1.630			0.80	1.757
0.35	1.640			0.85	1.790
0.40	1.650			0.90	1.847
0.45	1.661			0.95	1.917